An example of use of gas turbine engine compressor, which has been mastered in production and has good characteristics in a new product project
The development of a new gas turbine engine requires a lot of time and money spent on the design and testing its compressor, which has been shown as the most complex and time-consuming assembly unit of the engine. This article examines the potential application of the industry-developed engine co...
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| Format: | Article |
| Language: | English |
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Omsk State Technical University, Federal State Autonomous Educational Institution of Higher Education
2022-12-01
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| Series: | Омский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение" |
| Subjects: | |
| Online Access: | https://www.omgtu.ru/general_information/media_omgtu/journal_of_omsk_research_journal/files/arhiv/2022/%D0%A2.6%20%E2%84%964%20(%D0%90%D0%A0%D0%B8%D0%AD%D0%9C)/53-59%20%D0%93%D1%80%D0%B5%D1%85%D0%BD%D0%B5%D0%B2%20%D0%90.%20%D0%92..pdf |
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| _version_ | 1832572825088557056 |
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| author | A. V. Grekhnev |
| author_facet | A. V. Grekhnev |
| author_sort | A. V. Grekhnev |
| collection | DOAJ |
| description | The development of a new gas turbine engine requires a lot of time and money spent on the design
and testing its compressor, which has been shown as the most complex and time-consuming assembly
unit of the engine.
This article examines the potential application of the industry-developed engine compressors in the
designs of a new turbojet engine and a gas turbine compressor. The comparative analysis of the ideal
cycles of an augmented turbojet engine and a turbojet engine with a high-temperature combustor is
made. The advantage of the turbojet engine with a high-temperature combustor configuration over
the augmented turbojet engine configuration is shown. The high rates of jet-pipe gas velocity make a
turbojet engine with a high-temperature combustor suitable for supersonic cruise products. |
| format | Article |
| id | doaj-art-9a07fe140bfe47efbd78c430d24895e7 |
| institution | Kabale University |
| issn | 2588-0373 2587-764X |
| language | English |
| publishDate | 2022-12-01 |
| publisher | Omsk State Technical University, Federal State Autonomous Educational Institution of Higher Education |
| record_format | Article |
| series | Омский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение" |
| spelling | doaj-art-9a07fe140bfe47efbd78c430d24895e72025-02-02T07:14:36ZengOmsk State Technical University, Federal State Autonomous Educational Institution of Higher EducationОмский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение"2588-03732587-764X2022-12-0164535910.25206/2588-0373-2022-6-4-53-59An example of use of gas turbine engine compressor, which has been mastered in production and has good characteristics in a new product projectA. V. Grekhnev0Branch of the Public Joint Stock Company «UEC-Saturn» — Omsk Engine Design BureauThe development of a new gas turbine engine requires a lot of time and money spent on the design and testing its compressor, which has been shown as the most complex and time-consuming assembly unit of the engine. This article examines the potential application of the industry-developed engine compressors in the designs of a new turbojet engine and a gas turbine compressor. The comparative analysis of the ideal cycles of an augmented turbojet engine and a turbojet engine with a high-temperature combustor is made. The advantage of the turbojet engine with a high-temperature combustor configuration over the augmented turbojet engine configuration is shown. The high rates of jet-pipe gas velocity make a turbojet engine with a high-temperature combustor suitable for supersonic cruise products.https://www.omgtu.ru/general_information/media_omgtu/journal_of_omsk_research_journal/files/arhiv/2022/%D0%A2.6%20%E2%84%964%20(%D0%90%D0%A0%D0%B8%D0%AD%D0%9C)/53-59%20%D0%93%D1%80%D0%B5%D1%85%D0%BD%D0%B5%D0%B2%20%D0%90.%20%D0%92..pdfturbojet enginecompressorturbinemain combustion chamberhigh temperature combustion chamberafterburnerjet nozzleideal engine cycle |
| spellingShingle | A. V. Grekhnev An example of use of gas turbine engine compressor, which has been mastered in production and has good characteristics in a new product project Омский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение" turbojet engine compressor turbine main combustion chamber high temperature combustion chamber afterburner jet nozzle ideal engine cycle |
| title | An example of use of gas turbine engine compressor, which has been mastered in production and has good characteristics in a new product project |
| title_full | An example of use of gas turbine engine compressor, which has been mastered in production and has good characteristics in a new product project |
| title_fullStr | An example of use of gas turbine engine compressor, which has been mastered in production and has good characteristics in a new product project |
| title_full_unstemmed | An example of use of gas turbine engine compressor, which has been mastered in production and has good characteristics in a new product project |
| title_short | An example of use of gas turbine engine compressor, which has been mastered in production and has good characteristics in a new product project |
| title_sort | example of use of gas turbine engine compressor which has been mastered in production and has good characteristics in a new product project |
| topic | turbojet engine compressor turbine main combustion chamber high temperature combustion chamber afterburner jet nozzle ideal engine cycle |
| url | https://www.omgtu.ru/general_information/media_omgtu/journal_of_omsk_research_journal/files/arhiv/2022/%D0%A2.6%20%E2%84%964%20(%D0%90%D0%A0%D0%B8%D0%AD%D0%9C)/53-59%20%D0%93%D1%80%D0%B5%D1%85%D0%BD%D0%B5%D0%B2%20%D0%90.%20%D0%92..pdf |
| work_keys_str_mv | AT avgrekhnev anexampleofuseofgasturbineenginecompressorwhichhasbeenmasteredinproductionandhasgoodcharacteristicsinanewproductproject AT avgrekhnev exampleofuseofgasturbineenginecompressorwhichhasbeenmasteredinproductionandhasgoodcharacteristicsinanewproductproject |